×
验证码:
换一张
忘记密码?
记住我
CORC
首页
科研机构
检索
知识图谱
申请加入
托管服务
登录
注册
在结果中检索
科研机构
北京航空航天大学 [6]
长春光学精密机械与物... [3]
清华大学 [1]
西安光学精密机械研究... [1]
内容类型
期刊论文 [7]
会议论文 [4]
发表日期
2022 [1]
2020 [1]
2019 [1]
2018 [4]
2015 [1]
2012 [2]
更多...
×
知识图谱
CORC
开始提交
已提交作品
待认领作品
已认领作品
未提交全文
收藏管理
QQ客服
官方微博
反馈留言
浏览/检索结果:
共11条,第1-10条
帮助
已选(
0
)
清除
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
作者升序
作者降序
题名升序
题名降序
发表日期升序
发表日期降序
提交时间升序
提交时间降序
The Design of Cone and Pendulum Scanning Mode Using Dual-Camera with Multi-Dimensional Motion Imaging Micro-Nanosatellite
期刊论文
Remote Sensing, 2022, 卷号: 14, 期号: 18, 页码: 28
作者:
Z. Zhi
;
H. S. Qu
;
S. P. Tao
;
L. L. Zheng
;
S. P. Ying and H. Q. Zhu
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2023/06/14
Compact catadioptric optical system with long focal length large relative aperture and large field of view
会议论文
Beijing, PEOPLES R CHINA, 2020-11-30
作者:
Shen, Yang
;
Wang, Hu
;
Xue, Yaoke
;
Xie, Yongjie
;
Lin, Shangmin
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2021/06/04
Optical system design
Coaxial four reflection
Catadioptric system
Aberration compensation
Fabrication and preliminary testing of hydroxylammonium nitrate (HAN)-based ceramic microthruster for potential application of nanosatellites in constellation formation flying
期刊论文
MICROSYSTEM TECHNOLOGIES-MICRO-AND NANOSYSTEMS-INFORMATION STORAGE AND PROCESSING SYSTEMS, 2019, 卷号: 25, 页码: 4209-4217
作者:
Markandan, Kalaimani
;
Zhang, Zhe
;
Chin, Jitkai
;
Cheah, Kean How
;
Tang, Hai-Bin
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2019/12/30
Allocation Optimization Strategy for High-Precision Control of Picosatellites and Nanosatellites
期刊论文
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2018
作者:
Yang, Bo
;
Miao, Jun
;
Fan, Zichen
;
Long, Jun
;
Liu, Xuhui
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
A high-precision attitude coordinated control method using MEMS thruster for pico- and nano-satellite [一种皮纳卫星MEMS固体微推力器阵列联合姿态控制的高精度方法]
期刊论文
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2018, 卷号: 44, 页码: 1378-1386
作者:
Yang, B.
;
Li, J.
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Actuators
Attitude control
Costs
Flywheels
Global optimization
Nanosatellites
Numerical methods
Sliding mode control
Solid propellants
Spacecraft propulsion
Wheels
Allocation matrices
Attitude stability
Co-ordinated control
High-precision
Lyapunov stability
Microthruster
Optimal switching
Terminal sliding mode
Monte Carlo methods
Location awareness method for spot beam emitters
期刊论文
IET RADAR SONAR AND NAVIGATION, 2018, 卷号: 12, 页码: 1493-1499
作者:
Yang, Weicai
;
Chang, Qing
;
Li, Hui
;
Gao, Yang
;
Bao, Lina
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Equations of motion
Nanosatellites
Orbits
Location awareness
Location method
Low earth orbits
Measurement process
Radio frequencies
Realistic scenario
RF interference
Rf spectrum managements
Location
LOW-COST EPS FOR NANOSATELLITES CONSTELLATION OF BELT AND ROAD COUNTRIES
会议论文
FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III, 2018-01-01
作者:
Kerrouche, K. Dj. E.
;
Wang, L.
;
Aoudeche, A.
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2019/12/30
Orbit Injection Considerations for Cluster Flight of Nanosatellites
期刊论文
JOURNAL OF SPACECRAFT AND ROCKETS, 2015, 卷号: 52, 页码: 196-208
作者:
Wen, Changxuan
;
Zhang, Hao
;
Gurfil, Pini
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Design of a Miniature Axial Flux Flywheel Motor with PCB Winding for Nanosatellites
会议论文
2012
Wu J. F.
;
Ieee
收藏
  |  
浏览/下载:12/0
  |  
提交时间:2013/03/28
Design of a miniature axial flux flywheel motor with PCB winding for nanosatellites (EI CONFERENCE)
会议论文
2012 International Conference on Optoelectronics and Microelectronics, ICOM 2012, August 23, 2012 - August 25, 2012, Changchun, China
Wu J.
收藏
  |  
浏览/下载:34/0
  |  
提交时间:2013/03/25
This paper presents the design and analysis of an axial flux permanent-magnet (AFPM) machine for nanosatellites application. It is a miniature axial flux surface mounted permanent magnet flywheel motor
using a printed circuit board (PCB) stator winding. The PCB stator has simplified the design and construction and avoids unnecessary space
since size reduction has become one of the most important aspects of flywheel motor design for nanosatellites. The performances of the machine are estimated by combination method of three-dimensional (3D) electromagnetic finite element analysis (FEA) and approximate theoretical analysis. The back EMF and electromagnetic torque are derived. A comparison between the analysis and experimental measurement results of the prototype machine is also presented. Both simulated and experimental results show that the proposed motor would be an acceptable solution for the nanosatellite applications with advantages such as simple structure and low-cost
as multi-layer circuit board production techniques have made the production of printed circuit coils cheaper and easier. 2012 IEEE.
©版权所有 ©2017 CSpace - Powered by
CSpace